Separation of a supersonic turbulent boundary layer by a forward facing step
- 25 January 1971
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
- Theory of laminar viscous-inviscid interactions in supersonic flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1969
- Turbulent boundary-layer separation in front of a forward-facing step.AIAA Journal, 1967
- Supersonic separated and reattaching laminar flows. i - general theory and application to adiabatic boundary-layershock-wave interactionsAIAA Journal, 1964
- Fluctuating Wall Pressure under a Separated Supersonic FlowThe Journal of the Acoustical Society of America, 1964
- Separation of a Supersonic Turbulent Boundary LayerJournal of the Aeronautical Sciences, 1955
- Turbulent Boundary Layers in Adverse Pressure GradientsJournal of the Aeronautical Sciences, 1954
- On the Measurement of Surface Pressure with a Static ProbeJournal of the Aeronautical Sciences, 1953